GE CF34-3B1

Service difficulty reports · 5,402

Newest first. General aviation reporting is voluntary.

Query with SQL
duckdb -csv -c "SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy
  FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet'
  WHERE engine_model_key = 'CF343B1'
  ORDER BY difficulty_date DESC"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR SWIA200413054Frame · crackedDISCOVERED DURING C-CHECK INSPECTION, RIGHT SIDE FRAME STA 640 BETWEEN STR 9 AND STR 12 CRACKED. PARTS MADE IAW CRJ REO 601R-53-61-557. REPAIR PARTS INSTALLED IAW CRJ REO 601R-53-61-557 AT FR STA 640 BTWN STR 9 AND STR 12 RIGHT SIDE.Mar 9, 2004 · N412SW · Cndair CL6002B19 · Fuselage Main, FrameSDR SWIA200413045Frame · crackedMAIN FUSELAGE; FS 280.00; RBL 9; UPPER FLANGE CRACKED. REPAIRED IAW CRJ REO 601R-53-11-137 REV NC AND RII53-401.Mar 9, 2004 · N412SW · Cndair CL6002B19 · Fuselage Main, FrameSDR SWIA200413075Window · crackedLEFT WINDOW CRACKED AT 17,000 FT. INSTALLED SERVICEABLE LEFT WINDOW ASSEMBLY IAW CRJ MM 56-12-01 AND RII 56-402. NO LEAKS NOTED. P/N OFF: NP139322-001, S/N OFF: 02218H3041.Mar 8, 2004 · N934SW · Cndair CL6002B19 · Flight Compartment WindowsSDR SWIA200413162Seat Track · corrodedFUSELAGE SEAT TRACKS HAVE CORROSION FS 399 TO 599 + 96 LBL 9. DISCOVERED DURING C-CHECK INSPECTION. SEAT RAIL FS 409+126 TO 559+04 REPLACED. SEAT RAIL FS 559+04 TO 559+85 REPLACED.Mar 6, 2004 · N406SW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR SWIA200412988Computer · malfunctionedSTALL FAIL MESSAGE. REMOVED AND REPLACED STALL PROTECTION COMPUTER IAW CRJ MM 27-34. OPS CHECKS GOOD. STALL FAIL LIGHT ILLUMINATED LATER IN THE DAY AND STAYED ON FOR DURATION OF THE FLIGHT. CHECKED ASSOCIATED WIRING BEHIND STALL PROTECTION COMPUTER. NO DEMar 5, 2004 · N962SW · Cndair CL6002B19 · Stall Warning SystemSDR CA040511005Engine · fod(CAN) AFTER TAKEOFF THE CREW REPORTED SMOKE IN THE CABIN. AN EMEREGENCY WAS DECLARED AND THE AIRCRAFT RETURNED TO BASE AND MADE AN UNEVENTFUL LANDING. BOROSCOPE INSPECTION REVEALED FOD (FOD TYPE WAS NOT IDENTIFIED) FROM 1ST TO 7TH STAGE COMPRESSOR OF LT ENGINMar 2, 2004 · Cndair CL604 · Turbine Engine Compressor SectionSDR SWIA200412982Connector · damagedFLAPS EICAS PAGE (FLT CTRL) SHOWS FLAP DISCREP F20 INDICATES = 20 LT, 16 RT, F8 = 8 LT, 4 RT, F45 = 45 LT, 41 RT, F30 = 30 LT, 26 RT. NO ABNORMAL MSGS. A/C FLIES STRAIGHT. NO HANDLING PROBLEMS. FOUND CONNECTOR PIN HOLE 40 ON PLUG 211 WORN AND WILL NOT RETAFeb 24, 2004 · N903SW · Cndair CL6002B19 · Trailing Flap Position Indicating SystemSDR MASA200400100Accelerometer · unserviceableABORTED T/O DUE TO NR 1 ENG N2 VIB ICON ON EICAS. MX REPLACED THE NR 1 EVM AND A/C DEPARTED WITHOUT FURTHER INCIDENT.Feb 23, 2004 · N77302 · Cndair CL6002B19 · Engine Vibration AnalyzerSDR CA040316002Control Unit · failed(CAN) BLEED AIR OVERHEAT CONDITION (LT HAND) DOWNSTREAM OF ENG BLEED AIR SHUT OFF VALVE. WARNING WAS INTERMITTENT, BUT REMAINED ON. FOLLOWING AFM PROCEDURES, LT ENG WAS SHUT DOWN IN FLIGHT WHEN WARNING PERSISTED AFTER AFFECTED BLEED VALVE WAS CLOSED. AC WAS Feb 23, 2004 · Cndair CL604 · Central WarningSDR SWIA200412938Control Unit · malfunctionedSTAB TRIM 2 WILL NOT TEST CORRECTLY. ROCKER SWITCH DISENGAGES STAB 2. REMOVED AND REPLACED STAB MOTOR CONTROL UNIT AND HORIZONTAL ACTUATOR IAW MM 27-40-00, 27-48-00 & RII CARD 27-415.Feb 22, 2004 · N417SW · Cndair CL6002B19 · Stabilizer Control SystemSDR SWIA200413143Intercostal · crackedCRACKED INTERCOSTAL AT STA X484.00 BETWEEN LBL 27 AND LBL 36 (OUTBOARD). DISCOVERED DURING C-CHECK INSPECTION. REPAIRED INTERCOSTAL IAW REO 601R-53-41-059 REV A.Feb 20, 2004 · N923SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA200412922Servo · failedAUTOPILOT JERKS LEFT AND RIGHT MAINLY IN TURNS AND MOST PRONOUNCED WHEN SELECTING AND DE-SELECTING TURBULENCE BUTTON. REMOVED AND REPLACED RIGHT AUTO PILOT SERVO IAW 22-11-21. OPS CHECK GOOD. P/N: 622-4404-101, S/N OFF: 122.Feb 16, 2004 · N411SW · Cndair CL6002B19 · Autopilot Main ServoSDR SWIA200412923Control Unit · malfunctionedSPOILERON FAULT STATUS MESSAGE ON GROUND, UNABLE TO CLEAR WITH CIRCUIT BREAKERS. REMOVED AND REPLACED NR 1 SECU PER MM 27-61-05. OPS CHECK GOOD.Feb 15, 2004 · N438SW · Cndair CL6002B19 · Drag Control SystemSDR SWIA200412924Computer · malfunctionedDURING CLIMBOUT YAW DAMPER 2 DISENGAGED AND WOULD RESET FOR 2 TO 5 MINUTES AND THEN DISENGAGE. REMOVED AND REPLACED FCC 2 IAW 22-12-14. OPS CHECK GOOD.Feb 15, 2004 · N459SW · Cndair CL6002B19 · Autopilot SystemSDR VNAA0402007Strut · failedIN FLIGHT,GEAR WOULD NOT RETRACT. DURING PUSHBACK FROM GATE, NOSE GEAR WAS TURNED PAST ITS LIMIT. NOSE WHEEL STEERING WAS THEN REPORTED INOPERATIVE. MAINTENANCE INSPECTED AND REPLACED ELECTRO HYDRAULIC STEERING VALVE IAW MFG MM. OPERATIONAL CHECKS WERE PERFeb 14, 2004 · N218PS · Cndair CL6002B19 · Nose/Tail Landing GearSDR SWIA200412920Control Unit · malfunctionedAT CRUISE, RECEIVED A SPOILERONS CAUTION MSG ABOUT 1 MINUTE LATER, A FLT SPOILERS CAUTION MESSAGE ALONG WITH AN I/B GND SPLR FAULT MESSAGE. ON LANDING, THE SPOILERONS AND FLIGHT SPOILERS DEPLOYED ONLY, NO GROUND SPOILERS DEPLOYED. REMOVED AND REPLACED NR 2 SFeb 14, 2004 · N926SW · Cndair CL6002B19 · Drag Control SystemSDR SWIA200412921Control Unit · malfunctionedDURING FFOD CHECK ON STAB TRIM CH 2 AND MACH TRIM, THE STAB TRIM 2 WOULD NOT STAY ENGAGED DURING THE TEST. REPLACED HORIZONTAL STAB TRIM ACTUATOR AND MOTOR CONTROL UNIT IAW RJ MM 27-42-01, 27-42-05 AND RII CARD 27-415. OPS CHECKS GOOD. ACTUATOR P/N: 8396-3,Feb 14, 2004 · N912SW · Cndair CL6002B19 · Stabilizer Position IndicatingSDR A6WA200440022Carbon Seal · leakingIN FLIGHT RIGHT ENGINE OIL PRESSURE WARNING LIGHT ILLUMINATED. OIL PRESSURE FLUCTUATING BETWEEN 20-30 PSI. COMPLIED WITH QRH. ALL OTHER ENGINE INDICATIONS NORMAL. LANDED WITH RT ENGINE AT IDLE AT MCI. INSPECTED AND FOUND OIL COMING FROM GANG DRAIN. R & RFeb 14, 2004 · N424AW · Cndair CL6002B19 · Turbine Engine Oil SystemSDR VNAA0402006Pdu · failedIN FLIGHT, THE CREW RECEIVED A RIGHT HAND ENGINE THRUST REVERSER UNLOCK INDICATION AND RETURNED TO PIT. MAINTENANCE INSPECTED AND REPLACED THE POWER DRIVE UNIT IN ACCORDANCE WITH BOMBARDIER MAINTENANCE MANUAL 78-00-00. OPERATIONAL CHECKS WERE PERFORMED AND TFeb 13, 2004 · N215PS · Cndair CL6002B19 · Engine Thrust ReverserSDR VNAA0402005Warning System · activatedIN FLIGHT, THE CREW RECEIVED A RIGHT HAND EMERGENCY DOOR CAS MESSAGE. AIRCRAFT PRESSURE STAYED NORMAL. MAINTENANCE CONTROL, WITH THE CREW, THEN DEFERRED THE DOOR WITH 52-70-03 CAT C.Feb 11, 2004 · N226JS · Cndair CL6002B19 · Door Warning SystemSDR SWIA200412884Computer · malfunctionedYAW DAMPER (YD) 1 TRIPPED OFF IN CRUISE. RESET (REPEATEDLY), GOT PROGRESSIVELY WORSE DOWN TO 2 SECONDS BETWEEN RESETS AND FAILS. ASSOCIATED: AP TRIPS OFF WITH YD1, AI NR 1 BLANKS OUT AND MAG FLAG APPEARS WITH YD1. VSI NR 1 ERRONEOUS INDICATIONS - SHOWS UP Feb 10, 2004 · N965SW · Cndair CL6002B19 · Attitude and Direction Data SystemSDR VNAA0402004Sensor · dirtyDURING FLIGHT, THE CREW RECEIVED A RIGHT EMERGENCY DOOR ILLUMINATION AND YELLOW CAS MESSAGE. UPON ARRIVAL AT PHL, OUTSTATION MAINTENANCE FOUND CODE S42 IN THE PSEU. MAINTENANCE THEN CLEANED AND INSPECTED THE PROXY SENSOR AND TARGET IN ACCORDANCE WITH BOMBARDFeb 10, 2004 · N226JS · Cndair CL6002B19 · Door Warning SystemSDR SWIA200412883Pcu · malfunctionedON TAXI OUT, SPOILERONS FAULT STATUS MESSAGE. REMOVED AND REPLACED RIGHT SPOILERON OUTBOARD PCU AND SECU NR 1. OPS CHECK SATISFACTORY. LEAK CHECK SATISFACTORY IAW MM 27-60-03. PCU P/N: 49-164-06, S/N OFF: 01389.Feb 8, 2004 · N445SW · Cndair CL6002B19 · Drag Control SystemSDR ASOA04097Pump · cloggedFLT 4553 - DURING CRUISE FROM DTW-DFW, AT APPROXIMATELY 31,000 FEET THE CREW RECEIVED A RIGHT ENGINE LOW OIL PRESSURE WARNING MESSAGE. THE OIL PRESSURE FLUCTUATED BETWEEN 25-33 PSI OCCASIONALLY DROPPING BELOW 25 PSI AND THEN SLOWLY DECREASING. OIL TEMPERATURFeb 7, 2004 · N866AS · Cndair CL6002B19 · Turbine Engine Oil SystemSDR VNAA0402001Switch · out of adjustDURING FLIGHT, THE CREW RECEIVED AN EMERGENCY DOOR INDICATION AT 25,000 FEET, THE INDICATION WENT OFF AT 10,000 FEET. MAINTENANCE INSPECTED AND ADJUSTED THE RIGHT HAND EMERGENCY DOOR SWITCH IN ACCORDANCE WITH BOMBARDIER MAINTENANCE MANUAL 52-00-00. OPERATIONFeb 4, 2004 · N229PS · Cndair CL6002B19 · Door Warning SystemSDR SWIA200412855Pdu · malfunctionedFLAPS 1/2 SPEED MESSAGE. REPLACED FLAP POWER DRIVER UNIT IAW MM 27-52-01-000-801. OPS CHECK GOOD.Feb 2, 2004 · N941SW · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR VNAA0401016Connector · failedDURING FLIGHT, THE RIGHT HAND ENGINE WAS SURGING AND FLIGHT 2216 RETURNED TO DAY. MAINTENANCE INSPECTED AND CLEANED THE RIGHT HAND ENGINE CONNECTOR IN ACCORDANCE WITH BOMBARDIER MAINTENANCE MANUAL 71-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT Jan 30, 2004 · N206PS · Cndair CL6002B19 · Turbine Engine System WiringSDR VNAA0401015Pin · failedTHE CREW REPORTED THAT THE FLIGHT ATTENDANT PANEL'S EMERGENCY LIGHT SWITCH WAS NOT WORKING PROPERLY. MAINTENANCE INSPECTED AND REPLACED A PIN IN THE PANEL'S CONNECTOR IN ACCORDANCE WITH SMP. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FORJan 28, 2004 · N221PS · Cndair CL6002B19 · Light System WiringSDR VNAA0401014Outflow Valve · failedDURING CLIMB, CREW COULD NOT PRESURIZE AIRCRAFT. AIRCRAFT RETURNED TO PIT. MAINTENANCE INSPECTED AND REPLACED THE PRIMARY OUTFLOW VALVE IN ACCORDANCE WITH BOMBARDIER MAINTENANCE MANUAL 21-00-00. OPERATIONAL CHECKS WERE PERFORMED AND AIRCRAFT WAS RELEASED FOJan 27, 2004 · N209PS · Cndair CL6002B19 · Pressure Regulator/Outflow ValveSDR CA040127016Overheat Sensor · inoperative(CAN) LT 14TH DUCT MESSAGE ON EICAS AT 500 AGL (84 PERCENT N1) SHORTLY AFTER T/O, DUCT SHOWED RED BETWEEN COWL A/I AND WING A/I VALVES ON ANTI-ICE STATUS PAGE. CREW RETURNED, LANDED 700 KGS OVERWEIGHT.Jan 27, 2004 · Cndair CL6002B19 · Overheat DetectionSDR CA040205003Window · cracked(CAN) DURING CRUISE, FLIGHTDECK LT SIDE WINDOW CRACKED. FLIGHT WAS DIVERTED WHERE THE WINDOW WAS REPLACED. THE CRACKED WINDOW HAD BEEN FITTED SINCE THE A/C WAS NEW. THERE IS NO PRE OR POST SB FOR SIDE WINDOWS.Jan 26, 2004 · Cndair CL6002B19 · Flight Compartment WindowsSDR CA040208003Apu · leaking(CAN) FOR THE OVERNIGHT, THE FLIGHT CREW WERE ASKED TO LEAVE THE APU RUNNING TO PERMIT AIRCRAFT GROOMING. APPROXIMATELY ONE HOUR AFTER ARRIVAL, THE APU FIRE DETECTION SYSTEM PERFORMED AN AUTO SHUTDOWN AND APU FIRE BOTTLE WAS DEPLETED. GROUND/AIRCRAFT PERSONNJan 25, 2004 · Cndair CL6002B19 · APU Engine Fuel and ControlSDR MASA200400044Fan Blade · vibrationCREW REPORTED NR 1 ENGINE HIGH VIBE DURING TAKE-OFF. A/C RETURNED TO THE FIELD AND MX WAS CALLED. MX BORESCOPED THE ENGINE AND WAS GOOD. MX NOTICED SEVERAL FAN BLADES WITH CHIPS. MX REPLACED THE FAN BLADES. OP CHECKS GOOD.Jan 25, 2004 · N75991 · Cndair CL6002B19 · Turbine Engine Compressor SectionSDR MASA200400045Engine · hot startCREW REPORTED LEFT ENGINE HOT START. MX DRY MOTORED AND THAN STARTED THE ENG. OP CHECKS GOOD. NO PARTS USEDJan 25, 2004 · N17217 · Cndair CL6002B19 · Engine (Turbine/Turboprop)SDR VNAA0401013Controller · malfunctionedDURING CLIMB, CREW COULD NOT PRESSURIZE AIRCRAFT. AIRCRAFT RETURNED TO YOW. MAINTENANCE DEFERRED BOTH AUTO CABIN PRESSURE CONTROLLERS 21-31-1 CODE C.Jan 24, 2004 · N209PS · Cndair CL6002B19 · Cabin Pressure ControllerSDR SWIA200412829Computer · malfunctionedWITH THE AUTOPILOT ON, THE CONTROL YOKE JERKS FORWARD SHARPLY. THE JERK IS MILD DURING CRUISE INTERMITTENTLY. THE JERK IS MORE PRONOUNCED DURING THE DESCENT AND LEVEL OFF AT LOW ALTITUDE FOR THE APPROACH. REMOVED AND REPLACED NR 2 AHC COMPUTER. OPS CHECKS Jan 24, 2004 · N416SW · Cndair CL6002B19 · Attitude and Direction Data SystemSDR SWIA200412816Computer · malfunctionedRED FD ON BOTH PRIMARY FLIGHT DIRECTOR'S, FD1 FAIL STATUS MESSAGE AND YD1 INOP STATUS MESSSAGE IN FLIGHT. RETURNED TO SLC. REMOVED AND REPLACED NR 1 FCC 4000 CARD. OPS CHECKS GOOD IAW 22-11-00 AND 22-12-14.Jan 23, 2004 · N587SW · Cndair CL6002B19 · Autopilot SystemSDR VNAA0401012Warning Light · illuminatedDURING TAXI, CREW RECEIVED A CARGO DOOR LIGHT MESSAGE. AIRCRAFT THEN RETURNED TO BLOCK. MAINTENANCE THEN DEFERRED THE CARGO DOOR INDICATION IN ACCORDANCE WITH 52-70-4 CODE C.Jan 23, 2004 · N213PS · Cndair CL6002B19 · Door Warning SystemSDR SWIA200412797Bulb · inoperativeSECOND ROW OF CABIN EMERGENCY LIGHTS (CEILING) INOP. REMOVED AND REPLACED LIGHT BULB. OPS CHECK GOOD.Jan 21, 2004 · N906SW · Cndair CL6002B19 · Emergency LightingSDR A6WA200440008Engine · vibrationNR 1 ENGINE INDICATES VIB YELLOW CAUTION ON TAKEOFF ROLL BELOW 60 KNOTS. ABORTED TAKEOFF, NO VIBRATION FELT. REVIEWED HISTORY, PERFORMED TWO SEPARATE ENGINE POWER RUNS, NO VIBRATION NOTED. FAN BLADE INSPECTED, NO DISCREPANCIES. TAKEOFF WAS PERFORMED IN SEVJan 17, 2004 · N422AW · Cndair CL6002B19 · Engine (Turbine/Turboprop)SDR CA040116003Pcu · inoperative(CAN) REPEAT OF L1411710 UPON RT ENG START WITH HYD PUMPS IN AUTO RT FLT SPOILER HAS UNCOMMANDED DEPLOYMENT TO 50 DEG SLOWLY AND THEN RETRACTS TO ZERO . SPOILERS DO NOT OPERATE DURING THIS OCCURANCE REGARDLESS OF FLT SPOILER LEVER POSN. UNTIL RT SPOILER REACHEJan 16, 2004 · Cndair CL6002B19 · Drag Control SystemSDR A6WA200440006Skin · lightning strikeRIVET ON RT FUSELAGE SKIN AT FS 265.00 BETWEEN STRINGERS 22 AND 23 HAS LIGHTNING DAMAGE THAT EXTENDS BEYOND COUNTERSINK HOLE IN SKIN. (ADDTNL INFO-WO 59971 MWC 22) REMOVED FASTENER, ENLARGED FASTENER HOLE TO A NOMINAL .1875 DIAMETER, PERFORMED EDDY CURRENT TOJan 13, 2004 · N404AW · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR SWIA200412915Angle · crackedFS 625 LT INTERCOSTAL ANGLE CRACKED STR 14L. DISCOVERED DURING C-CHECK INSPECTION. ANGLE REPLACED IAW CRJ SRM 51-40-11, 51-42-06.Jan 12, 2004 · N409SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA200412916Angle · crackedFS 662 LT FIRE WALL SHUT-OFF INTERCOSTAL ANGLE CRACKED. DISCOVERED DURING C-CHECK INSPECTION. REPLACED ANGLE IAW CRJ SRM 51-40-11, 51-42-06.Jan 12, 2004 · N409SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA200412917Angle · crackedFS 589 CARGO DOOR FLOOR LANDING PLATE TRANSVERSE BEAM ANGLE LBL 44 CRACKED. DISCOVERED DURING C-CHECK INSPECTION. REPLACED ANGLE IAW CRJ SRM 51-40-11-11, 51-42-06, 51-42-21, 51-23-00 & RII 53-401.Jan 12, 2004 · N409SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA200412918Angle · crackedFS 625 RT INTERCOSTAL ANGLE STR 14R CRACKED. DISCOVERED DURING C-CHECK INSPECTION. ANGLE REPLACED IAW CRJ SRM 51-40-11, 51-42-06.Jan 12, 2004 · N409SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA200412919Angle · crackedFS 605 CARGO DOOR LANDING PLATE TRANSVERSE BEAM LBL 44 ANGLE CRACKED. DISCOVERED DURING C-CHECK INSPECTION. REPLACED ANGLE IAW CRJ SRM 51-40-11, 51-42-06, 51-42-21, 51-23-00 & RII 53-401.Jan 12, 2004 · N409SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR MASA200400015Fuel Control · out of adjustASH 2670 PHL-STL, NR 1 ENGINE SHUT DOWN ON DESCENT WHEN THROTTLES SELECTED TO IDLE. CREW FOLLOWED CHECK LIST AND RESTARTED ENGINE. ENGINE PERFORMED PROPERLY THE REST OF THE DESCENT. MX PERFORMED ENGINE RUN AND FUEL CONTROL ADJUSTMENTS PER FIM. A/C CONTINUEJan 8, 2004 · N75992 · Cndair CL6002B19 · Fuel Controlling SystemSDR SWIA200412802Actuator · malfunctionedSTAB CH 1 INOP STATUS MESSAGE WILL NOT GO OUT. REMOVED AND REPLACED HSTA AND MCU SYSTEM. OPS CHECK GOOD PER CRJ MM 27-12-01. MCU P/N: 7062-3, S/N OFF 1126.Jan 7, 2004 · N906SW · Cndair CL6002B19 · Stabilizer Control SystemSDR CA040126008Switch · failed(CAN) 30 MINS OUT, FL260 RUDDER TRIM FAILED, INADVERTENT AND SUDDEN DISPLACEMENT TO HALFWAY TO FULL NOSE LT. DECLARED EMERGENCY, UNEVENTFUL LANDING. RUDDER TRIM FAILED. REMOVED AND REPLACED RUDDER TRIM SWITCH. OPS CHECKS REQUIRED WHEN PANEL REINSTALLED IAW27-Jan 6, 2004 · Cndair CL6002B19 · Rudder Control System
Back to GE CF34-3B1